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Study of Airfoil Deflections for Unsteady Aerodynamics Optimization in Pitching Airfoils

Camber deflection concepts for a VR-12 rotorcraft airfoil were studied for the optimization of unsteady aerodynamics, including dynamic stall conditions and wing–wing interactions during pitching. The designs are based on deflections of the leading edge and trailing edge sections of the airfoil. The...

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Principais autores: William Refling, Charles Fabijanic, Thomas Sprengeler, Yildirim Bora Suzen, Jordi Estevadeordal
Format: Artigo
Sprog:Inglês
Udgivet: MDPI AG 2025-02-01
Serier:Applied Sciences
Fag:
airfoil aerodynamics
pitching flow control
separation
dynamic stall
particle image velocimetry
numerical simulations
Online adgang:https://www.mdpi.com/2076-3417/15/5/2455
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